View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 66389U 26145.41435382 +.00000000 +00000-0 +43013-3 0 00007
2 66389 53.1587 220.4137 0001141 70.1496 289.9628 15.30203165 06
| Epoch (UTC): | 25 May 2026 09:56:40 |
| Eccentricity: | 0.0001141 |
| inclination: | 53.1587° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 220.4137° |
| argument of perigee: | 70.1496° |
| revolutions per day: | 15.30203165 |
| mean anomaly at epoch: | 289.9628° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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